DE2303382C3 - Turbostrahltriebwerk - Google Patents
TurbostrahltriebwerkInfo
- Publication number
- DE2303382C3 DE2303382C3 DE19732303382 DE2303382A DE2303382C3 DE 2303382 C3 DE2303382 C3 DE 2303382C3 DE 19732303382 DE19732303382 DE 19732303382 DE 2303382 A DE2303382 A DE 2303382A DE 2303382 C3 DE2303382 C3 DE 2303382C3
- Authority
- DE
- Germany
- Prior art keywords
- hollow shaft
- shaft
- rotor
- sections
- pressure compressor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/026—Shaft to shaft connections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7202693A FR2168938B1 (da) | 1972-01-27 | 1972-01-27 |
Publications (3)
Publication Number | Publication Date |
---|---|
DE2303382A1 DE2303382A1 (de) | 1973-08-02 |
DE2303382B2 DE2303382B2 (de) | 1980-07-03 |
DE2303382C3 true DE2303382C3 (de) | 1981-04-30 |
Family
ID=9092530
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19732303382 Expired DE2303382C3 (de) | 1972-01-27 | 1973-01-24 | Turbostrahltriebwerk |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE2303382C3 (da) |
FR (1) | FR2168938B1 (da) |
GB (1) | GB1357712A (da) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2046843B (en) * | 1979-04-17 | 1983-01-26 | Rolls Royce | Gas turbine engines-de-icing-icing |
FR2621554B1 (fr) * | 1987-10-07 | 1990-01-05 | Snecma | Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe |
US4860534A (en) * | 1988-08-24 | 1989-08-29 | General Motors Corporation | Inlet particle separator with anti-icing means |
GB9120113D0 (en) * | 1991-09-20 | 1992-09-23 | Short Brothers Plc | Thermal antiicing of aircraft structures |
FR2950928B1 (fr) * | 2009-10-02 | 2011-12-09 | Snecma | Cone d'entree autodegivrant pour turbomachine d'aeronef |
ITCO20110017A1 (it) * | 2011-05-19 | 2012-11-20 | Nuovo Pignone Spa | Sistema di turbina a gas integrato e metodo |
FR2998620B1 (fr) | 2012-11-29 | 2018-04-06 | Safran Aircraft Engines | Capot de turbomachine apte a recouvrir un cone de soufflante |
FR3025551B1 (fr) * | 2014-09-05 | 2019-08-23 | Safran Aircraft Engines | Arbre de turbomachine |
CN107061013B (zh) * | 2017-03-30 | 2019-05-24 | 中国航发沈阳发动机研究所 | 一种用于发动机进口旋转整流帽罩的热气防冰方法 |
CN112302725B (zh) * | 2020-09-18 | 2022-07-26 | 中国航发四川燃气涡轮研究院 | 一种紧凑型航空发动机高压转子连接结构 |
FR3143545A1 (fr) * | 2022-12-16 | 2024-06-21 | Safran Nacelles | Capot d’une turbomachine d’aéronef comprenant une interface centrale de préhension |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2757857A (en) * | 1951-06-19 | 1956-08-07 | United Aircraft Corp | Locking means between compressor and turbine |
FR1520460A (fr) * | 1967-01-11 | 1968-04-12 | Snecma | Perfectionnements aux turboréacteurs à flux multiples |
GB1210202A (en) * | 1969-03-06 | 1970-10-28 | Rolls Royce | Gas turbine engine |
-
1972
- 1972-01-27 FR FR7202693A patent/FR2168938B1/fr not_active Expired
-
1973
- 1973-01-17 GB GB245873A patent/GB1357712A/en not_active Expired
- 1973-01-24 DE DE19732303382 patent/DE2303382C3/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2303382B2 (de) | 1980-07-03 |
FR2168938A1 (da) | 1973-09-07 |
FR2168938B1 (da) | 1974-12-13 |
GB1357712A (en) | 1974-06-26 |
DE2303382A1 (de) | 1973-08-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C3 | Grant after two publication steps (3rd publication) | ||
8339 | Ceased/non-payment of the annual fee |